Completed projects

In 2015-2019 Advance Engineering specialists implemented a number of consulting projects and development projects, completed agreements for 70 large customers - machine-building enterprises of the Russian Federation. Among them: UEC JSC, UAC PJSC, Russian Helicopters JSC, Kamaz PJSC, Power Machines PJSC, Sinara Transport Machines JSC, FSUE NAMI, FSUE «Central Aviation Institute motor engineering named after P.I. Baranova» and others.

 

Advance Engineering actively cooperates with higher educational institutions of Russia, such as:

  • FSAEI HE "South Ural State University (National Research University)";

  • FSBEI HE “Ufa State Aviation Technical University”;

  • FSBEI HE “Perm National Research Polytechnic University” and others.

Collaboration with training centers allows us to apply their experience and knowledge in carrying out research and development work, to test samples of materials and equipment, and also to perform design work that requires the use of significant computing power.

In 2019, together with the Federal State Autonomous Educational Institution of Higher Education “UrFU named after the first President of Russia B.N. Yeltsin ”, the Engineering Center of Mechanical Engineering Digital Technologies was opened, which has a complex of specialized laboratories, unique stands, high-tech equipment and a staff of qualified specialists already actively involved in the ongoing complex projects of Advance Engineering.

 

 

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OUR WORKS:

 

AUTOMATION OF STRENGTH MULTI-VARIANT CALCULATIONS OF GTE ELEMENTS FOR DESIGNERS

Purpose:

  • Acceleration of design of gas turbine engine elements due to automation of calculations

Result:

  • The calculation check time for one geometry option is reduced by 25%

WEIGHT OPTIMIZATION OF THE CASE OF THE GTE COMBUSTION CHAMBER IN ANSYS WORKBENCH

Purpose:

  • Reduce the mass of the combustion chamber housing

Result:

  • Weight reduced by 7%
  • Optimized design

 

 

VIRTUAL TESTS OF THE GTE COMBUSTION CHAMBER FOR COMPLIANCE WITH EUROPEAN STANDARDS

Purpose:

  • Reduced costly field tests

Result:

  • The volume of field tests has been reduced;
  • The technique was verified by the results of tests of an autonomous five-burner compartment.

VIRTUAL TESTS AND CALCULATIONS FOR DURABILITY OF CARRYING ELEMENTS OF A/M KAMAZ SUSPENSION SYSTEM

Purpose:

  • Development of virtual test methods

Result:

  • A model of the dynamics of a car with a flexible frame along a "virtual" range
  • Automation and simplified interface

 

 

HYDRODYNAMIC CALCULATION OF THE GEAR PUMP TAKING INTO ACCOUNT CAVITATION

Purpose:

  • Creation of a gear pump simulation technique

Result:

  • A methodology has been developed for determining pump performance, location and extent of cavitation zones
  • The pressure characteristic was calculated and a low-order model was built for the gear pump

 

DEVELOPMENT OF A METHOD OF MODELING DEPARTURE OF GRAVEL FROM UNDER THE
TRAIN

Purpose:

  • Optimization of the protection of the suspension elements of the train from the impact of gravel particles

Result:

  • Reduced design time for the protection of train suspension elements
  • A technique has been developed to optimize the aerodynamic shape in order to minimize the departure of gravel from under the train
 

 

 

 

ELECTRIC TRAIN WAGON CONDITIONING SYSTEM

Purpose:

  • Optimization of the heating system for the interior of the electric train

Result:

  • Minimized heterogeneity of temperature and air velocity in the cabin
  • Reduced analysis time of one design option by several times

 

DEVELOPMENT OF A METHOD FOR EVALUATING AERODYNAMIC CHARACTERISTICS OF A HELICOPTER FUSELAGE

Purpose:

  • Development of a methodology for numerical simulation of the external flow around a helicopter fuselage

Result:

  • Reduced the number of full-scale tests in the wind tunnel
  • The aerodynamic characteristics of the fuselage of the Ansat helicopter and its individual elements

 

 

 

MODELING OF THE AIR CONDITION SYSTEM OF THE PILOT CABIN AND THE TRANSPORT CABIN OF THE HELICOPTER

Purpose:

  • Develop a calculation methodology

Result:

  • Prepared calculation procedure in FloEFD software
  • Problem solving time ~ 3 days
  • Duration of calculations on three grids ~ 12 hours
  • The employees of the enterprise were trained to work in the FloEFD software package

 

 

SEND APPLICATION FOR THE PROJECT

We will help to implement the projects of your enterprise. Describe the problem that you want to solve, and our specialist will contact you.

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